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ad 1999-411-140 b r1 pdf

Federal Register Airworthiness Directives Airbus Airplanes. This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June, 文档格式:PDF 浏览次数:3 This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement Manufacturer(s): Airbus (formerly Airbus Industrie) Applicability: Airbus A319-111,.

EASA Recommended master template ad.easa.europa.eu

[4910-13-P] DEPARTMENT OF TRANSPORTATION. Each document posted on the site includes a link to the corresponding official PDF file on govinfo.gov. This Airworthiness Directives; Airbus Airplanes. France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19,, DGAC [Direction Générale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (“AD 2000-12-13”)] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different unsafe.

Supersedure: This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement 1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via …

GSAC AIRWORTHINESS DIRECTIVE ref. : 1999-411-140(B) R1 Page nВ° 2 REASON The Airworthiness Directive 97-153-100(B)R1 requires application of AFM TR 4.03.00/02 because of an FMGS software anomaly that lead pilot to reinforce his monitoring of the aircraft and that may lead the aircraft to be out of his flight path. DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different

DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different Each document posted on the site includes a link to the corresponding official PDF file on govinfo.gov. This Airworthiness Directives; Airbus Airplanes. France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19,

The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations . 3 office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. (FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference

1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via … DGAC [Direction Générale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (“AD 2000-12-13”)] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different unsafe

1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via … 1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via …

The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations . 3 office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. Supersedure: This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement

The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations . 3 office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different

Numéro de l’AD AD Number Authority Objet / Subject Autorité Traduction Translation CN originales Original AD's 2014-0205 R1 Correction AIRBUS – Avions A380 - [Correction] Wings – Movable Flap Track Fairing Number 4 Pivot Brackets – Inspection / Repair / Replacement EASA 2016-0130-E DASSAULT AVIATION– Avions-Falcon 900 EX, Falcon Numéro de l’AD AD Number Authority Objet / Subject Autorité Traduction Translation CN originales Original AD's 2014-0205 R1 Correction AIRBUS – Avions A380 - [Correction] Wings – Movable Flap Track Fairing Number 4 Pivot Brackets – Inspection / Repair / Replacement EASA 2016-0130-E DASSAULT AVIATION– Avions-Falcon 900 EX, Falcon

(FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June

Numéro de l’AD AD Number Authority Objet / Subject Autorité Traduction Translation CN originales Original AD's 2014-0205 R1 Correction AIRBUS – Avions A380 - [Correction] Wings – Movable Flap Track Fairing Number 4 Pivot Brackets – Inspection / Repair / Replacement EASA 2016-0130-E DASSAULT AVIATION– Avions-Falcon 900 EX, Falcon Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard. This AD requires identification of potentially affected FMGCs,

DGAC [Direction Générale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (“AD 2000-12-13”)] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different unsafe Numéro de l’AD AD Number Authority Objet / Subject Autorité Traduction Translation CN originales Original AD's 2014-0205 R1 Correction AIRBUS – Avions A380 - [Correction] Wings – Movable Flap Track Fairing Number 4 Pivot Brackets – Inspection / Repair / Replacement EASA 2016-0130-E DASSAULT AVIATION– Avions-Falcon 900 EX, Falcon

DGAC [Direction Générale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (“AD 2000-12-13”)] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different unsafe (FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference

Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard. This AD requires identification of potentially affected FMGCs, 1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via …

Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard. This AD requires identification of potentially affected FMGCs, DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different

Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard. This AD requires identification of potentially affected FMGCs, DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different

[4910-13-P] DEPARTMENT OF TRANSPORTATION

ad 1999-411-140 b r1 pdf

47084 Federal Register /Vol. 82 No. 195/Wednesday. Each document posted on the site includes a link to the corresponding official PDF file on govinfo.gov. This Airworthiness Directives; Airbus Airplanes. France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19,, DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different.

Numéro de l’AD Traduction AD Number Authority

ad 1999-411-140 b r1 pdf

[4910-13-P] DEPARTMENT OF TRANSPORTATION. Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard. This AD requires identification of potentially affected FMGCs, 1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via ….

ad 1999-411-140 b r1 pdf


GSAC AIRWORTHINESS DIRECTIVE ref. : 1999-411-140(B) R1 Page nВ° 2 REASON The Airworthiness Directive 97-153-100(B)R1 requires application of AFM TR 4.03.00/02 because of an FMGS software anomaly that lead pilot to reinforce his monitoring of the aircraft and that may lead the aircraft to be out of his flight path. (FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference

GSAC AIRWORTHINESS DIRECTIVE ref. : 1999-411-140(B) R1 Page n° 2 REASON The Airworthiness Directive 97-153-100(B)R1 requires application of AFM TR 4.03.00/02 because of an FMGS software anomaly that lead pilot to reinforce his monitoring of the aircraft and that may lead the aircraft to be out of his flight path. 文档格式:PDF 浏览次数:3 This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement Manufacturer(s): Airbus (formerly Airbus Industrie) Applicability: Airbus A319-111,

1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via … This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June

GSAC AIRWORTHINESS DIRECTIVE ref. : 1999-411-140(B) R1 Page n° 2 REASON The Airworthiness Directive 97-153-100(B)R1 requires application of AFM TR 4.03.00/02 because of an FMGS software anomaly that lead pilot to reinforce his monitoring of the aircraft and that may lead the aircraft to be out of his flight path. This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June

(FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations . 3 office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.

文档格式:PDF 浏览次数:3 This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement Manufacturer(s): Airbus (formerly Airbus Industrie) Applicability: Airbus A319-111, Supersedure: This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement

Numéro de l’AD AD Number Authority Objet / Subject Autorité Traduction Translation CN originales Original AD's 2014-0205 R1 Correction AIRBUS – Avions A380 - [Correction] Wings – Movable Flap Track Fairing Number 4 Pivot Brackets – Inspection / Repair / Replacement EASA 2016-0130-E DASSAULT AVIATION– Avions-Falcon 900 EX, Falcon (FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference

Each document posted on the site includes a link to the corresponding official PDF file on govinfo.gov. This Airworthiness Directives; Airbus Airplanes. France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different

Supersedure: This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement DGAC [Direction Générale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (“AD 2000-12-13”)] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different unsafe

This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June DGAC [Direction Générale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (“AD 2000-12-13”)] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different unsafe

(FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference 文档格式:PDF 浏览次数:3 This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement Manufacturer(s): Airbus (formerly Airbus Industrie) Applicability: Airbus A319-111,

GSAC AIRWORTHINESS DIRECTIVE ref. : 1999-411-140(B) R1 Page nВ° 2 REASON The Airworthiness Directive 97-153-100(B)R1 requires application of AFM TR 4.03.00/02 because of an FMGS software anomaly that lead pilot to reinforce his monitoring of the aircraft and that may lead the aircraft to be out of his flight path. DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different

Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a runway excursion due to an unexpected thrust increase leading to an unstable approach performed using the current flight management and guidance computer (FMGC) standard. This AD requires identification of potentially affected FMGCs, This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June

Each document posted on the site includes a link to the corresponding official PDF file on govinfo.gov. This Airworthiness Directives; Airbus Airplanes. France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, (FMGC) standard. This AD requires identification of potentially affected FMGCs, replacement of any affected FMGC, and applicable concurrent actions. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 15, 2017. The Director of the Federal Register approved the incorporation by reference

1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via … 1 [Federal Register Volume 82, Number 195 (Wednesday, October 11, 2017)] [Rules and Regulations] [Pages 47084-47091] From the Federal Register Online via …

文档格式:PDF 浏览次数:3 This AD supersedes DGAC France AD 1998-226-119(B)R1 dated 22 January 2000 and AD 1999-411-140(B)R1 dated 13 May 2000. ATA 22 – Auto Flight – Flight Management and Guidance Computer – Replacement Manufacturer(s): Airbus (formerly Airbus Industrie) Applicability: Airbus A319-111, Numéro de l’AD AD Number Authority Objet / Subject Autorité Traduction Translation CN originales Original AD's 2014-0205 R1 Correction AIRBUS – Avions A380 - [Correction] Wings – Movable Flap Track Fairing Number 4 Pivot Brackets – Inspection / Repair / Replacement EASA 2016-0130-E DASSAULT AVIATION– Avions-Falcon 900 EX, Falcon

DGAC [Direction G[eacute]n[eacute]rale de l'Aviation Civile] France issued AD 1999-411-140(B)R1 [which corresponds to FAA AD 2000-12-13, Amendment 39-11791 (65 FR 37845, June 19, 2000) (``AD 2000-12-13'')] and AD 1998-226-119(B)R1 [which corresponds to FAA AD 98-19-08, Amendment 39-10750 (63 FR 50503, September 22, 1998)] to address different This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The Civile] France issued AD 1999–411–140(B)R1 [which corresponds to FAA AD 2000–12–13, Amendment 39–11791 (65 FR 37845, June